Available results summarized; effects of aspect ratio and Mach number studied, and subsonic values for derivatives included in investigation of Mach number effects; non-linearities in sideslip variation of yawing and rolling moments; effects of combining wing and body indicated for two of derivatives.


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    Title :

    Theoretical lateral-stability derivatives for wings at supersonic speeds


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Jones, A.L. (author)


    Publication date :

    1950


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Stability derivatives of triangular wings at supersonic speeds

    Ribner, H.S. / Malvestuto, Jr., F.S. | Engineering Index Backfile | 1948


    Stability derivatives of triangular wings at supersonic speeds

    Ribner, H.S. / Malvestuto, Jr., F.S. | Engineering Index Backfile | 1948


    Stability derivatives of triangular wings at supersonic speeds

    Ribner, Herbert S. / Malvestuto, Frank S. | TIBKAT | 1948


    Stability derivatives of triangular wings at supersonic speeds

    Ribner, Herbert S / Malvestuto, Frank S , Jr | NTRS | 1948


    Stability Derivatives of Triangular Wings at Supersonic Speeds

    H. S. Ribner / F. S. Malvesstuto | NTIS | 1948